G5 K10-00280-30

Garmin - Electronic Flight Instrument
Part Number :

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G5
FEATURES
  • All-glass Primary or Backup Flight Instrument with Optional Autopilot Capability
  • Flush Mount Kit available under P/N 115-02733-00
  • Sunlight readable
  • 3.5 inch LCD color display
  • Sized to fit standard 3 1/8 inch instrument cutout
  • Rotary knob on the unit allows for easy adjustments
  • Can be used as a primary EFIS attitude indicator or DG/HSI display (see P/N chart below for DG/HSI models) — or as a fully integrated backup flight instrument for G3X™, G3X Touch™ or other Experimental/LSA glass cockpits
  • Provides standalone or backup autopilot control, allowing coupled GPS approaches to be flown or continued in the event of a primary display loss
  • Built-in GPS receiver and optional GPS antenna available
  • Replaces traditional electromechanical backup instruments
  • Combines flight information in one display, consolidates situational reference for aircraft attitude, vertical speed, altitude, airspeed, slip/skid, and baro setting
  • When integrated with the G3X system, the G5 can provide heading, course deviation, flight director cues, autopilot mode annunciation, turn coordination, glideslope/glidepath, altitude and airspeed bug settings, and more
  • Teamed with Garmin autopilot servos and the GMC 307/305 mode controller interface, the G5 provides backup or standalone autopilot function
  • Can be connected through a serial port to a Garmin portable GPS such as aera 660/795/796 to enable the autopilot to couple laterally to the flight plan and vertically to support VNAV descents to pattern altitude
  • G5 has 2 pilot-selectable main page formats: a PFD page and a DG (directional gyro) or HSI (horizontal situation indicator) page
  • VHF or GPS navigation inputs are required to drive the HSI display; for GPS interface, an optional GAD™ 29 navigation data adapter is required
  • Optional lithium-ion battery backup sustains G5 with up to 4 hours of emergency power
  • Designed specifically for the experimental amateur-built (EAB) and light sport aircraft (LSA) markets
  • Dual G5 installation offers reversionary display capability plus the added redundancy of dual ADAHRS and dual back-up batteries
  • An STC permission letter will be granted for each aircraft in which the G5 for certified aircraft is installed
    • To retrieve this STC letter, the single-use registration code included in the standard kit must be submitted by following the outlined steps
  • View the FAA Policy Statement on Replacement of Vacuum Driven Attitude Indicators in 14 CFR, Part 23/CAR 3 Airplanes
 
SPECIFICATIONS
Electrical: 14 or 28 VDC aircraft power Size: Unit: 3.4"W x 3.6"H x 2.6"D, Display: 3.5" diagonal
Weight: Unit: 13.3 oz Resolution: 320 x 240 pixels (QVGA), LED backlit color LCD
Receiver: High-sensitivity GPS Max IndicateD AirSpeed: 300 kts
altitude Range: -1,400 - +30,000 feet Vertical Speed Range: +/- 20,000 feet/minute
Pitch/roll Range: +/- 360º backup battery option: Rechargeable lithium-ion
battery life: Up to 4 hours    
Part Number Primary flight instrument:
010-01485-00 Unit Only, Catalog PN
K10-00280-00 Primary Attitude Indictor, Standard Kit
K10-00280-20 Heading Indicator (DG) or HSI, Standard Kit
K10-00280-30 HSI with GPS Nav Interface Adapter, Standard Kit

 

K10-00280-00
- Electronic Flight Instrument
Price Condition Delivery
$2,149.00 NEW OUTRIGHT IN STOCK

SEA Repair Capabilities: No

K10-00280-20
- DG/HSI Electronic Flight Instrument
Price Condition Delivery
$2,449.00 NEW OUTRIGHT IN STOCK

SEA Repair Capabilities: No

K10-00280-30
- DG/HSI w/ GAD29B Nav Interface
Price Condition Delivery
$2,975.00 NEW OUTRIGHT IN STOCK

SEA Repair Capabilities: No

Click on a question below to see the answer. If you have a question about this model that is not answered below, please contact questions@seaerospace.com

As of June 2017, the Garmin G5 (all versions) do not have the ability to interface to an autopilot.

As of June 2017, the G5 has not been approved as the standby instrument in the G1000 cockpit.

For the G5 DG/HSI version with nav interface (PN K10-00280-30), only Garmin nav/GPS radios will interface to the G5.  This includes the Garmin GNC-255 series, SL30, GNS-430/530 series, and GTN-650/750 series navigators.

As of September 2017, the Garmin G5 electronic flight instrument is not a replacement for the KI-256 flight command indicator. 

 

The DG/HSI version of the G5 can interface to a variety of autopilots such as the King KFC-150/200 to provide heading and course error to the autopilot.  The G5 can interface to select autopilots for coupled flight in heading and nav modes with a compatible navigation source.

well.  The KI-256 is not simply an attitude gyro/indicator.  It supplies attitude data to KFC autopilots and is a flight director as well.

Yes in November 2017, Garmin released a PMAd flush mount adapter plate for either single or dual installations. Part Number for ordering is 115-02733-00.  List Price is $99.95.

 

The G5 electronic instrument is capable of operating as a primary attitude indicator, backup attitude indicator with primary rate-of-turn indicator, DG or HSI.

 

The STC approves the installation of the G5 in an existing instrument panel. In the attitude application, the G5 can replace an existing vacuum attitude indicator or rate-of-turn indicator. The G5 can also replace existing vacuum driven DGs or existing HSI, either standalone or in combination with a G5 attitude display. 


The G5 is designed to be installed into a standard 3” instrument hole in place of existing indicators . Other primary flight instruments remain in their current approved locations. Please note that the G5 cannot replace an existing primary attitude indicator that has a Flight Director. However, if the existing attitude indicator is interfaced to the autopilot and it does not include Flight Director, the existing attitude indicator can be moved to the rate of turn indicator location and G5 installed as the primary attitude indicator. Also, for installations that do not install a G5 as the replacement primary attitude indicator, the G5 can be installed as a second attitude indicator in place of the existing rate of turn indicator. However, if the existing rate of turn indicator is interfaced with the autopilot, it cannot be replaced by a G5. The G5 can only be installed in the locations specified in the STC. It is an installer’s responsibility to ensure the installation limitations are considered prior to modifying an aircraft.